| 摘要 |
The present invention relates to an unmanned aerial vehicle having a loading function and, more specifically, to a weight unbalance correction method, a weight unbalance measurement device, and a weight unbalance correction device for an unmanned aerial vehicle. The weight unbalance correction method comprises: a step of loading an object in a multicopter; a step of measuring a weight unbalance value; and a step of coordinating thrust between propellers on the basis of the measured weight unbalance value. |
